SpaceAtlas Space Object Data
NASA JPL SBDB · 2023 VG3

2023 VG3

2023 VG3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.415 AU it takes 1.68 yr to circle the Sun.

Apollo Observations: 182
Orbital Period · P
1.68 yr
v(q)
38.4 km/s
v(Q)
16.3 km/s
Diameter · ≈
0.11 km
TJ
4.6
Eccentricity · e
0.4026

Orbit and dynamics

Between its closest point (0.845 AU) and its farthest (1.985 AU), the heliocentric distance changes by 1.14 AU over every revolution.

One full revolution takes 1.68 yr (615 days), computed from the semi-major axis of 1.415 AU.

The high eccentricity (0.403) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 15.34° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 38.4 km/s at perihelion and falls to 16.3 km/s at aphelion.

Because q < 1 AU and Q > 1 AU, this orbit geometrically intersects the region of Earth's orbit.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 22.64 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.11 km.

Observation record and orbit quality

Astrometry from 182 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3514 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

About these computed values

Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

Orbital Parameters

Semi-Major Axis
1.415 AU
Eccentricity
0.4026
Perihelion
0.845 AU
Aphelion
1.984679 AU
Inclination
15.34°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
145.22°

Orbit diagram

The Sun sits at the focus (orange). Earth's orbit is the grey circle at 1 AU. The red dot marks the object's position at the catalog epoch.

3D orbit (interactive)

Drag to rotate; scroll or pinch to zoom. The Sun is at the focus (orange), Earth's orbit is the grey ring at 1 AU, and the red dot marks the object's current position.

Close approaches

Predicted close approaches to Earth, from NASA's Center for Near-Earth Object Studies (CNEOS).

Date (UTC)Miss distanceVelocity
2029-Feb-24 21:35 0.280301 AU
41932409 km
8.21 km/s
2029-Apr-29 15:15 0.266925 AU
39931381 km
8.55 km/s
2034-May-02 12:12 0.174835 AU
26154979 km
14.39 km/s
2039-May-15 01:25 0.400029 AU
59843422 km
22.52 km/s
2050-Nov-17 09:47 0.398895 AU
59673820 km
24.23 km/s
2055-Dec-02 14:13 0.085979 AU
12862309 km
15.72 km/s
2060-Dec-22 19:18 0.151412 AU
22650977 km
9.23 km/s
2061-May-11 19:42 0.358121 AU
53574118 km
8.71 km/s
2065-Nov-19 15:33 0.462069 AU
69124577 km
8.35 km/s
2066-Apr-28 05:59 0.163743 AU
24495656 km
10.80 km/s
2071-May-08 17:38 0.248540 AU
37181113 km
18.31 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
— km
Albedo
—
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
22.64

Orbit Quality

RMS
0.35142
Condition
6
Orbit ID
—
Data source: NASA JPL Small-Body Database · NASA CNEOS. Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

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